NSN 9540-01-478-9725
Part Details | STRUCTURAL ANGLE
9540-01-478-9725 A structural shape fabricated from a ferrous or nonferrous material and resembling the letter L in cross-sectional form. The edges may have a bulb, be rounded, and the inside corner may have a fillet.
Alternate Parts: HS1004DD630525, HS1004DD63-0525, 9540-01-478-9725, 01-478-9725, 9540014789725, 014789725
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | OCT 04, 2000 | 01-478-9725 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-478-9725
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HS1004DD63-0525 | 8V613 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 9540-01-478-9725
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | J$DRG |
| LENGTH | 5.781 INCHES NOMINAL |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| OVERALL WIDTH | 1.500 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.062 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| END ITEM IDENTIFICATION | APACHE HELICOPTER |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | EXTRUDED ANGLE - UNEQUAL LEG, ALUMINUM ALLOY |